{
  "$type": "site.standard.document",
  "description": "An air intake (36) for an aircraft propulsion system (10) includes an air inlet duct (54) and a flow control device (120). The air inlet duct (54) includes an interior surface (52) and an intake inlet (60). The interior surface (52) extends from the intake inlet (60). The interior surface (52)…",
  "path": "/patents/1392612",
  "publishedAt": "2025-12-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D33/02",
    "PRATT & WHITNEY CANADA [CA]"
  ],
  "textContent": "An air intake (36) for an aircraft propulsion system (10) includes an air inlet duct (54) and a flow control device (120). The air inlet duct (54) includes an interior surface (52) and an intake inlet (60). The interior surface (52) extends from the intake inlet (60). The interior surface (52) forms and surrounds an inlet flow passage (62) through the air inlet duct (54). The intake inlet (60) includes a top side (108), a bottom side (110), a first lateral side (112), and a second lateral side (114). Each of the first lateral side (112) and the second lateral side (114) extend between and to the top side (108) and the bottom side (110). The flow control device (120) is disposed inside the air inlet duct (54) at the first lateral side (112). The flow control device (120) is configured to form an asymmetrical shape of the intake inlet (60) at the first lateral side (112) relative to the second lateral side (114).",
  "title": "SYSTEMS AND METHODS FOR CONTROLLING AN INTAKE INLET SHAPE OF A PROPULSION SYSTEM AIR INTAKE"
}